EP0159169A2 - A process for joining different kinds of synthetic resins - Google Patents

A process for joining different kinds of synthetic resins Download PDF

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Publication number
EP0159169A2
EP0159169A2 EP19850302432 EP85302432A EP0159169A2 EP 0159169 A2 EP0159169 A2 EP 0159169A2 EP 19850302432 EP19850302432 EP 19850302432 EP 85302432 A EP85302432 A EP 85302432A EP 0159169 A2 EP0159169 A2 EP 0159169A2
Authority
EP
European Patent Office
Prior art keywords
synthetic resin
plate
laser beam
article
contact surface
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP19850302432
Other languages
German (de)
French (fr)
Other versions
EP0159169A3 (en
Inventor
Toshihisa Terasawa
Hideo Nakamata
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP59070606A external-priority patent/JPS60214929A/en
Priority claimed from JP59072256A external-priority patent/JPS60214931A/en
Application filed by Toyota Motor Corp filed Critical Toyota Motor Corp
Publication of EP0159169A2 publication Critical patent/EP0159169A2/en
Publication of EP0159169A3 publication Critical patent/EP0159169A3/en
Withdrawn legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1635Laser beams characterised by the way of heating the interface at least passing through one of the parts to be joined, i.e. laser transmission welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C37/00Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/0078Measures or configurations for obtaining anchoring effects in the contact areas between layers
    • B29C37/0082Mechanical anchoring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1677Laser beams making use of an absorber or impact modifier
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/3404Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint
    • B29C65/3408Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint comprising single particles, e.g. fillers or discontinuous fibre-reinforcements
    • B29C65/3412Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint comprising single particles, e.g. fillers or discontinuous fibre-reinforcements comprising fillers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/3404Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint
    • B29C65/344Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint being a woven or non-woven fabric or being a mesh
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/303Particular design of joint configurations the joint involving an anchoring effect
    • B29C66/3034Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/341Measures for intermixing the material of the joint interlayer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • B29C66/712General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined the composition of one of the parts to be joined being different from the composition of the other part
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721Fibre-reinforced materials
    • B29C66/7214Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72143Fibres of discontinuous lengths
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
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    • B29C65/1606Ultraviolet [UV] radiation, e.g. by ultraviolet excimer lasers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
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    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/3472Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint
    • B29C65/3484Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint being non-metallic
    • B29C65/3492Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint being non-metallic being carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
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    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
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    • B29C66/80General aspects of machine operations or constructions and parts thereof
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    • B29K2105/206Meshes, lattices or nets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2309/00Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08Glass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2707/00Use of elements other than metals for preformed parts, e.g. for inserts
    • B29K2707/04Carbon

Definitions

  • the present invention relates to a process for joining differing kinds of synthetic resin to each other, and more particularly to a process for joining them using the heat of a laser beam.
  • each of the synthetic resins has a contact surface thereon.
  • a metal mesh is disposed on the contact surfaces of the synthetic resins, and the mesh is sandwiched between both of the synthetic resins.
  • both of the contact surfaces of the synthetic resins are melted by the heat of the mesh.
  • Pressure then is applied to the outsides of the synthetic resins to press them together, and the synthetic resins are cooled.
  • one of the synthetic resins is joined to the other of the synthetic resins.
  • both synthetic resins normally are the same kind of synthetic resins so that both will have the same melting point, and so that they will blend easily into one another. If different kinds of synthetic resins are used, they may have differing melting points and may not blend easily into one another.
  • a connecting wire is disposed between both of the contact surfaces of the synthetic resins to supply electricity to heat the mesh. Connecting the wire to the mesh between the synthetic resins requires an undesirably high amount of manual labor.
  • each of the synthetic resins has a contact surface thereon, and a bonding compound is disposed between both of the contact surfaces of the synthetic resins.
  • the bonding compound normally is solid and is melted by heat, typically produced by applying high frequency or supersonic waves to the bonding compound. These waves also preferably melt the synthetic resins slightly to improve bonding. After a compressive force is applied to the synthetic resins, the synthetic resins are cooled. As a result of the second conventional process, one of the synthetic resins is joined to the other.
  • the synthetic resins again should be the same kind of synthetic resin, this time so that the bonding compound has the same adhesive properties for bonding to both synthetic resins.
  • the bonding compound may have differing adhesive properties as to the different kinds of synthetic resin. Accordingly, the adhesive strength of the bond to one kind of synthetic resin may be different from the adhesive strength of the bond to a different kind of synthetic resin, i. e., one bond may have a weak adhesive strength. Further, in the second conventional process with different synthetic resins, the synthetic resins may not both be melted by the heat of the high frequency or supersonic waves.
  • FIG. 11 shows a third conventional process for mechanically joining different kinds of synthetic resins.
  • a first plate 51 is mounted on a second plate 52.
  • the first plate 51 is made of polypropylene resin
  • the second plate 52 is made of polyethylene resin.
  • the first plate 51 has a first hole 511
  • the second plate 52 has a second hole 521 which is congruent with the first hole 511 of the first plate 51.
  • a washer 54 is mounted on the first plate 51, and a screw 55 is inserted into a hole of the washer 54, the first hole 511 and the second hole 521. As a result, the first plate 51 is joined mechanically to the second plate 52.
  • the first hole 511 must be opened in the first plate 51, and the second hole 521 must be opened in the second plate 52. Then, the screw 55 must be inserted.
  • Each of these steps is undesirably labor intensive. Further, the screw 55 projects from both of the first plate 51 and the second plate 52, marring the appearance of the final product.
  • the first plate 51 or the second plate 52 may be torn at the first hole 511 or at the second hole 521, respectively.
  • the present invention has been developed in view of the facts as described above, and its object is to provide a process for joining different kinds of synthetic resins which enables secure joining of different kinds of synthetic resins.
  • a process for joining different kinds of synthetic resins includes several steps.
  • a first step includes providing a first kind of synthetic resin, which can store up the heat from a laser beam.
  • a second step includes setting a second kind of synthetic resin on a first kind of synthetic resin.
  • a second contact surface of the second kind of synthetic resin is in contact with a first contact surface of the first kind of synthetic resin.
  • the second kind of synthetic resin can transmit the laser beam.
  • a third step includes exposing an outer surface of the second kind of synthetic resin to the laser beam.
  • the second kind of synthetic resin transmits the laser beam, and the first kind of synthetic resin stores up the heat of the laser beam.
  • the second contact surface of the second kind of synthetic resin is heated by the heat which is stored up in the first kind of synthetic resin.
  • the first contact surface of the first kind of synthetic resin and the second contact surface of the second kind of synthetic resin are melted by the heat which is stored up in the first kind of synthetic resin. While melted, they are pressed together, and cooled. Thus, the first contact surface of the first kind of synthetic resin is joined securely to the second contact surface of the second kind of synthetic resin.
  • the outer surface of. the second kind of synthetic resin does not have any scars, because the second kind of synthetic resin simply transmits the laser beam and the heat of the laser. beam is stored up in the first kind of synthetic resin.
  • a first step of a process for joining different kinds of synthetic resins includes providing a first plate 1 made of a first kind of synthetic resin which can store up the heat of a laser beam.
  • the first kind of synthetic resin can be styrene acrylonitrile copolymer including 0.1 wt% carbon black as an additive.
  • the first plate 1 of this composition is black.
  • the styrene acrylonitrile copolymer with carbon black transmits only a little of a Nd:YAG(Nd +3 :Y 3 Al 5 O 12 ) laser beam and therefore can store up (absorb) most of the heat of the total amount of the laser beam.
  • this composition will transmit only about 4% of the beam.
  • the first kind of synthetic resin may be polypropylene resin which includes carbon black as an additive.
  • a second step of the process includes setting a second plate 2 on the first plate 1.
  • the second plate 2 is made of a second kind of synthetic resin.
  • the second plate 2 has a second contact surface 21 which is in contact with a first contact surface 11 of the first plate 1.
  • the second kind of synthetic resin can transmit most of the laser beam, and preferably is polypropylene resin without any absorptive additive. As shown in FIG. 9, when the wavelength of the Nd:YAG laser beam is 1.06p m, the polypropylene resin without any additive can transmit about 75% of the total amount of the Nd:YAG laser beam.
  • the second kind of synthetic resin may be styrene acrylonitrile copolymer, 6-nylon resin or 66-nylon resin, all without any absorptive additives.
  • the color of the plate 2 is milky white.
  • a third step of the process includes setting a nozzle 4 of the laser beam on an outer surface of the second plate 2, and exposing the outer surface of the second plate 2 to the laser beam.
  • the laser beam radiates from the nozzle 4 through a convex lens 41, and an end of the nozzle 4 preferably is in contact with the outer surface of the second plate 2.
  • the second plate 2 transmits the laser beam, and the first plate 1 stores up the heat of the laser beam.
  • the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2 are melted by the heat which is stored up in the first plate 1.
  • a plurality of projections and a plurality of recesses are formed on the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2, because the laser beam is dispersed in the second plate 2 during transmission. Due to this dispersion, the laser beam concentrates on a plurality of spots which are located on the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2, and the laser beam melts a plurality of the spots. If the end of the nozzle 4 is not in contact with the outer surface of the second plate 2, a larger plurality of the recesses may be formed by moving the nozzle 4 along the outer surface of the second plate 2 during irradiation by the laser beam.
  • the most suitable laser beam is a Nd:YAG laser beam
  • other laser beams including: Nd:glass laser beam; ruby laser beam; helium:neon (He:Ne) gas laser beam; krypton (Kr) gas laser beam; argon (Ar) gas laser beam; hydrogen (H 2 ) gas laser beam and nitrogen CN 2 ) gas laser beam.
  • a suitable wavelength of the laser beam for joining different kinds of synthetic resins is about 1.06 pm and less.
  • the wavelength of the laser beam is more than 1.06 pm, the first kind of synthetic resin cannot be joined to the second kind of synthetic resin, because the second kind of synthetic resin cannot transmit the laser beam.
  • the laser beam should be from 5W through 100W in power in order to melt the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2.
  • the generating power of the laser beam is less than 5W, the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2 cannot be melted by the heat of the laser beam which is stored up in the first plate 1.
  • the generating power of the laser beam is more than 100W, the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2 may vaporize or may be transmuted, so that the first plate 1 cannot be joined to the second plate 2.
  • a fourth step of the process includes applying a downward compressive force "F" to the outer surface of the second plate 3 and the first plate 1 during exposing the second plate 2 to the laser beam.
  • the melted first kind of synthetic resin of the first plate 1 is pressed into the plurality of recesses of the second contact surface 21 of the second plate 2.
  • the melted second kind of synthetic resin of the second plate 2 is pressed into the plurality of recesses of the first contact surface 1 of the first plate 1.
  • a plurality of projections of the first contact surface 11 of the first plate 1 and a plurality of projections of the second contact surface 21 of the second plate 2 are formed.
  • the force "F 1 " preferably is applied to the second plate 2 through the nozzle 4 of the laser beam, though the downward compressive force "F” may be applied to the second plate 2 through a different device, and while or after the second plate 2 is being exposed to the laser beam.
  • a fifth step of the process includes stopping irradiation by the laser beam, and removing the nozzle 4 of the laser beam from the outer surface of the second plate 2. Concurrently, in the fifth step of the process, the downward compressive force "F 1 " is removed from the second plate 2. Alternatively, the downward compressive force "F 1 " may be removed from the second plate 2 after the nozzle 4 of the laser beam is removed from the outer surface of the second plate 2.
  • a sixth step of the process includes cooling the first plate 1 and the second plate 2, leaving the plurality of the projections of the first contact surface 11 of the first plate 1 engaged securely with the plurality of the recesses of the second contact surface 21 of the second plate 2, and vice-versa.
  • the first kind of synthetic resin can be securely joined to the second kind of synthetic resin.
  • FIG. 6 and FIG. 7 show a fifth step of a second embodiment of a process according to the invention for joining different kinds of synthetic resins.
  • Most of steps of the process in the second embodiment are the same as steps of the process in the first embodiment which is described above, however, the second embodiment has several differences. Description will be given hereunder of the several differences in the second embodiment.
  • a first kind of synthetic resin of a first plate 101 is styrene acrylonitrile copolymer.
  • the styrene acrylonitrile copolymer is reinforced with 20 wt% glass filler 102, and the styrene acrylonitrile copolymer includes 0.1 wt% carbon black as an additive.
  • the filler 102 of the first kind of synthetic resin may be a metal filier or a carbon filler instead of the glass filler.
  • the styrene acrylonitrile copolymer can transmit only a little of a Nd:YAG(Nd +3 :Y 3 Al 5 O 12 ) laser beam. Whan the wavelength of the laser beam is 1.06 pm, the reinforced styrene acrylonitrile copolymer can transmit about 4% of a total amount of the Nd:YAG laser beam. Therefore, the styrene acrylonitrile copolymer can store up most of the heat of the total amount of the laser beam.
  • a second kind of synthetic resin of a second plate 2 is polypropylene resin which does not include any absorptive additives. As shown in FIG. 9, when the wavelength of the Nd:YAG laser beam is 1.06 pm, the polypropylene resin without any absorptive additives can transmit about 75% of the total amount of the Nd:YAG laser beam.
  • a third step of the process includes setting a nozzle 4 of the laser beam on an outer surface of the second plate 2, and exposing the outer surface of the second plate 2 to the laser beam.
  • the laser beam radiates from the nozzle 4 through a convex lens 41, and an end of the nozzle 4 is in contact with the outer surface of the second plate 2.
  • the second plate 2 transmits the laser beam, and the first plate 101 stores up the heat of the laser beam. Therefore, the first contact surface 11 of the first plate 101 and the second contact surface 21 of the second plate 2 are melted by the heat which is stored up in the first plate 101.
  • the glass filler 102 of the first plate 101 cannot be melted by the heat of the laser beam, and the glass filler 102 therefore floats in the first kind of synthetic resin melted from the first plate 1 and the second kind of synthetic resin melted for the second plate 2 because the glass filler has a higher melting point than melting points of the first kind of synthetic resin and the second kind of synthetic.
  • a plurality of the fibers of the glass filler 102 will have ends in the first plate 101 and opposite ends in the second plate 2. Accordingly, some of the glass filler securely connects the first plate 101 to the second plate 2.
  • the cohesiveness between the first plate 101 and the' second plate 2 increases as the wt% of the glass filler increases.
  • the data in FIG. 10 was obtained by joining the preferred first and second kinds of synthetic resins by the heat of a Nd:YAG laser beam, whose generating power is 87W and whose wavelength is 1.06 pm.
  • the first kind of synthetic resin can be joined securely to the second kind of synthetic resin through the glass filler 102.
  • one kind of synthetic resin can be joined securely to a different kind of synthetic resin without any mechanical devices.
  • Further techniques for joining different kinds of synthetic resins may be found in the applications owned by applicant's assignee, filed in the European Patent Office concurrently with the present application and all entitled "A Process for Joining Different Kinds of Synthetic Resins".

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  • Engineering & Computer Science (AREA)
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  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
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Abstract

A process for joining a first kind of synthetic resin (1, 101) to a second kind of synthetic resin (2) includes several steps. A first step is providing the first kind of synthetic resin (1, 101), which may include fillers (102), e. g., glass fibers. A second step is setting a second contact surface (21) of the second kind of synthetic resin (2) on a first contact surface (11) of the first kind of synthetic resin (1, 101). A third step is exposing an outer surface of the second kind of synthetic resin (2) to a laser beam. The second kind of synthetic resin (2) transmits the laser beam to the first kind of synthetic resin (1, 101 which stores up heat of the laser beam. The second contact surface (21) of the second kind of synthetic resin (2) and the first contact surface (11) of the first kind of synthetic resin (1, 101) are melted by the heat of the laser beam. A plurality of projections and a plurality of recesses are formed on both the first contact surface (11) of the first kind of synthetic resin (1, 101) and the second contact surface (21) of the second kind of synthetic resin (2). A plurality of the projections of the first kind of synthetic resin (1, 101) engage with a plurality of the recesses of the second kind of synthetic resin (2). If fillers (102) are provided, at least some of them (102) will extend between the first and second synthetic resins (1, 101, 2). Accordingly, the second kind of synthetic resin (2) is securely joined to the first kind of synthetic resin (1, 101).

Description

  • The present invention relates to a process for joining differing kinds of synthetic resin to each other, and more particularly to a process for joining them using the heat of a laser beam.
  • In a first conventional process for physically joining synthetic resins, each of the synthetic resins has a contact surface thereon. A metal mesh is disposed on the contact surfaces of the synthetic resins, and the mesh is sandwiched between both of the synthetic resins. When the mesh is heated, both of the contact surfaces of the synthetic resins are melted by the heat of the mesh. Pressure then is applied to the outsides of the synthetic resins to press them together, and the synthetic resins are cooled. As a result of this first conventional process, one of the synthetic resins is joined to the other of the synthetic resins.
  • In this first conventional process, both synthetic resins normally are the same kind of synthetic resins so that both will have the same melting point, and so that they will blend easily into one another. If different kinds of synthetic resins are used, they may have differing melting points and may not blend easily into one another.
  • Further, in the first conventional process, a connecting wire is disposed between both of the contact surfaces of the synthetic resins to supply electricity to heat the mesh. Connecting the wire to the mesh between the synthetic resins requires an undesirably high amount of manual labor.
  • In a second conventional process for chemically joining synthetic resins, each of the synthetic resins has a contact surface thereon, and a bonding compound is disposed between both of the contact surfaces of the synthetic resins. The bonding compound normally is solid and is melted by heat, typically produced by applying high frequency or supersonic waves to the bonding compound. These waves also preferably melt the synthetic resins slightly to improve bonding. After a compressive force is applied to the synthetic resins, the synthetic resins are cooled. As a result of the second conventional process, one of the synthetic resins is joined to the other.
  • In the second conventional process, the synthetic resins again should be the same kind of synthetic resin, this time so that the bonding compound has the same adhesive properties for bonding to both synthetic resins. If different kinds of synthetic resins are used, the bonding compound may have differing adhesive properties as to the different kinds of synthetic resin. Accordingly, the adhesive strength of the bond to one kind of synthetic resin may be different from the adhesive strength of the bond to a different kind of synthetic resin, i. e., one bond may have a weak adhesive strength. Further, in the second conventional process with different synthetic resins, the synthetic resins may not both be melted by the heat of the high frequency or supersonic waves.
  • FIG. 11 shows a third conventional process for mechanically joining different kinds of synthetic resins. As shown in FIG. 11, a first plate 51 is mounted on a second plate 52. The first plate 51 is made of polypropylene resin, and the second plate 52 is made of polyethylene resin. The first plate 51 has a first hole 511, and the second plate 52 has a second hole 521 which is congruent with the first hole 511 of the first plate 51. A washer 54 is mounted on the first plate 51, and a screw 55 is inserted into a hole of the washer 54, the first hole 511 and the second hole 521. As a result, the first plate 51 is joined mechanically to the second plate 52.
  • However, in the third conventional process, the first hole 511 must be opened in the first plate 51, and the second hole 521 must be opened in the second plate 52. Then, the screw 55 must be inserted. Each of these steps is undesirably labor intensive. Further, the screw 55 projects from both of the first plate 51 and the second plate 52, marring the appearance of the final product. In addition, when tension is applied to the first plate 51 and the second plate 52 in the horizontal direction in FIG. 11, the first plate 51 or the second plate 52 may be torn at the first hole 511 or at the second hole 521, respectively.
  • The present invention has been developed in view of the facts as described above, and its object is to provide a process for joining different kinds of synthetic resins which enables secure joining of different kinds of synthetic resins.
  • To accomplish the above-described object, a process for joining different kinds of synthetic resins includes several steps.
  • A first step includes providing a first kind of synthetic resin, which can store up the heat from a laser beam. A second step includes setting a second kind of synthetic resin on a first kind of synthetic resin. A second contact surface of the second kind of synthetic resin is in contact with a first contact surface of the first kind of synthetic resin. The second kind of synthetic resin can transmit the laser beam. A third step includes exposing an outer surface of the second kind of synthetic resin to the laser beam. The second kind of synthetic resin transmits the laser beam, and the first kind of synthetic resin stores up the heat of the laser beam. As a result, the second contact surface of the second kind of synthetic resin is heated by the heat which is stored up in the first kind of synthetic resin. Accordingly, the first contact surface of the first kind of synthetic resin and the second contact surface of the second kind of synthetic resin are melted by the heat which is stored up in the first kind of synthetic resin. While melted, they are pressed together, and cooled. Thus, the first contact surface of the first kind of synthetic resin is joined securely to the second contact surface of the second kind of synthetic resin.
  • Further, the outer surface of. the second kind of synthetic resin does not have any scars, because the second kind of synthetic resin simply transmits the laser beam and the heat of the laser. beam is stored up in the first kind of synthetic resin.
  • Furthermore, neither the first kind of synthetic resin nor the second kind of synthetic resin can easily be torn, because neither has any holes therein.
  • Other objects and novel features of this invention will become more apparent from the description which follows, taken in conjunction with the accompanying drawings, and in which:
    • FIG. 1 is a cross-sectional view showing a second step of a first embodiment of a process according to the present invention;
    • FIG. 2 is a cross-sectional view showing a third step of the process;
    • FIG. 3 is a cross-sectional view showing a fourth step of the process;
    • FIG. 4 is a cross-sectional view showing a fifth step of the process;
    • FIG. 5 is an enlarged view of a portion of FIG. 4 showing a first contact surface of a first kind of synthetic resin which is joined to a second contact surface of a second kind of synthetic resin;
    • FIG. 6 is a cross-sectional view showing a fourth step of a second embodiment of a process according to the present invention, in which a first kind of synthetic resin includes fillers;
    • FIG. 7 is an enlarged view of a portion of FIG. 6 showing a first contact surface of the first kind of synthetic resin which is joined to a second contact surface of a second kind of synthetic resin;
    • FIG. 8 is a diagram showing the transmittance of 20 wt% glass filler reinforced styrene acrylonitrile copolymer with 0.1 wt% carbon black;
    • FIG. 9 is a diagram showing the transmittance of polypropylene without any additives;
    • FIG. 10 is a diagram showing the tensile strength of glass filler reinforced styrene acrylonitrile copolymer; and
    • FIG. 11 is a cross-sectional view showing a third conventional process.
  • Referring to FIG. 1, a first step of a process for joining different kinds of synthetic resins includes providing a first plate 1 made of a first kind of synthetic resin which can store up the heat of a laser beam. For example, the first kind of synthetic resin can be styrene acrylonitrile copolymer including 0.1 wt% carbon black as an additive. The first plate 1 of this composition is black. As shown in FIG. 8, the styrene acrylonitrile copolymer with carbon black transmits only a little of a Nd:YAG(Nd+3:Y3Al5O12) laser beam and therefore can store up (absorb) most of the heat of the total amount of the laser beam. At 1.06 pm, for example, this composition will transmit only about 4% of the beam. Alternatively, the first kind of synthetic resin may be polypropylene resin which includes carbon black as an additive.
  • Returning to FIG. 1, a second step of the process includes setting a second plate 2 on the first plate 1. The second plate 2 is made of a second kind of synthetic resin. The second plate 2 has a second contact surface 21 which is in contact with a first contact surface 11 of the first plate 1.
  • The second kind of synthetic resin can transmit most of the laser beam, and preferably is polypropylene resin without any absorptive additive. As shown in FIG. 9, when the wavelength of the Nd:YAG laser beam is 1.06p m, the polypropylene resin without any additive can transmit about 75% of the total amount of the Nd:YAG laser beam. Alternatively, the second kind of synthetic resin may be styrene acrylonitrile copolymer, 6-nylon resin or 66-nylon resin, all without any absorptive additives. The color of the plate 2 is milky white.
  • As shown in FIG. 2, a third step of the process includes setting a nozzle 4 of the laser beam on an outer surface of the second plate 2, and exposing the outer surface of the second plate 2 to the laser beam. The laser beam radiates from the nozzle 4 through a convex lens 41, and an end of the nozzle 4 preferably is in contact with the outer surface of the second plate 2.
  • When the outer surface of the second plate 2 is exposed to the laser beam, the second plate 2 transmits the laser beam, and the first plate 1 stores up the heat of the laser beam. As a result, the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2 are melted by the heat which is stored up in the first plate 1.
  • A plurality of projections and a plurality of recesses are formed on the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2, because the laser beam is dispersed in the second plate 2 during transmission. Due to this dispersion, the laser beam concentrates on a plurality of spots which are located on the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2, and the laser beam melts a plurality of the spots. If the end of the nozzle 4 is not in contact with the outer surface of the second plate 2, a larger plurality of the recesses may be formed by moving the nozzle 4 along the outer surface of the second plate 2 during irradiation by the laser beam.
  • With the preferred resins, the most suitable laser beam is a Nd:YAG laser beam, however, other laser beams may be used, including: Nd:glass laser beam; ruby laser beam; helium:neon (He:Ne) gas laser beam; krypton (Kr) gas laser beam; argon (Ar) gas laser beam; hydrogen (H2) gas laser beam and nitrogen CN2) gas laser beam.
  • With the preferred resins, a suitable wavelength of the laser beam for joining different kinds of synthetic resins is about 1.06 pm and less. When the wavelength of the laser beam is more than 1.06 pm, the first kind of synthetic resin cannot be joined to the second kind of synthetic resin, because the second kind of synthetic resin cannot transmit the laser beam.
  • With the preferred resins, the laser beam should be from 5W through 100W in power in order to melt the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2. When the generating power of the laser beam is less than 5W, the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2 cannot be melted by the heat of the laser beam which is stored up in the first plate 1. When the generating power of the laser beam is more than 100W, the first contact surface 11 of the first plate 1 and the second contact surface 21 of the second plate 2 may vaporize or may be transmuted, so that the first plate 1 cannot be joined to the second plate 2.
  • As shown in FIG. 3, a fourth step of the process includes applying a downward compressive force "F" to the outer surface of the second plate 3 and the first plate 1 during exposing the second plate 2 to the laser beam. As best seen in FIG. 5, the melted first kind of synthetic resin of the first plate 1 is pressed into the plurality of recesses of the second contact surface 21 of the second plate 2. Similarly, the melted second kind of synthetic resin of the second plate 2 is pressed into the plurality of recesses of the first contact surface 1 of the first plate 1. Thus, a plurality of projections of the first contact surface 11 of the first plate 1 and a plurality of projections of the second contact surface 21 of the second plate 2 are formed. The force "F1" preferably is applied to the second plate 2 through the nozzle 4 of the laser beam, though the downward compressive force "F" may be applied to the second plate 2 through a different device, and while or after the second plate 2 is being exposed to the laser beam.
  • As shown in FIG.4, a fifth step of the process includes stopping irradiation by the laser beam, and removing the nozzle 4 of the laser beam from the outer surface of the second plate 2. Concurrently, in the fifth step of the process, the downward compressive force "F 1" is removed from the second plate 2. Alternatively, the downward compressive force "F1" may be removed from the second plate 2 after the nozzle 4 of the laser beam is removed from the outer surface of the second plate 2.
  • A sixth step of the process includes cooling the first plate 1 and the second plate 2, leaving the plurality of the projections of the first contact surface 11 of the first plate 1 engaged securely with the plurality of the recesses of the second contact surface 21 of the second plate 2, and vice-versa.
  • Therefore, by this process, the first kind of synthetic resin can be securely joined to the second kind of synthetic resin.
  • FIG. 6 and FIG. 7 show a fifth step of a second embodiment of a process according to the invention for joining different kinds of synthetic resins. Most of steps of the process in the second embodiment are the same as steps of the process in the first embodiment which is described above, however, the second embodiment has several differences. Description will be given hereunder of the several differences in the second embodiment.
  • A first kind of synthetic resin of a first plate 101 is styrene acrylonitrile copolymer. The styrene acrylonitrile copolymer is reinforced with 20 wt% glass filler 102, and the styrene acrylonitrile copolymer includes 0.1 wt% carbon black as an additive. Alternatively, the filler 102 of the first kind of synthetic resin may be a metal filier or a carbon filler instead of the glass filler.
  • As shown in FIG. 8, the styrene acrylonitrile copolymer can transmit only a little of a Nd:YAG(Nd+3:Y3Al5O12) laser beam. Whan the wavelength of the laser beam is 1.06 pm, the reinforced styrene acrylonitrile copolymer can transmit about 4% of a total amount of the Nd:YAG laser beam. Therefore, the styrene acrylonitrile copolymer can store up most of the heat of the total amount of the laser beam.
  • A second kind of synthetic resin of a second plate 2 is polypropylene resin which does not include any absorptive additives. As shown in FIG. 9, when the wavelength of the Nd:YAG laser beam is 1.06 pm, the polypropylene resin without any absorptive additives can transmit about 75% of the total amount of the Nd:YAG laser beam.
  • A third step of the process includes setting a nozzle 4 of the laser beam on an outer surface of the second plate 2, and exposing the outer surface of the second plate 2 to the laser beam. The laser beam radiates from the nozzle 4 through a convex lens 41, and an end of the nozzle 4 is in contact with the outer surface of the second plate 2.
  • When the outer surface of the second plate 2 is exposed to the laser beam, the second plate 2 transmits the laser beam, and the first plate 101 stores up the heat of the laser beam. Therefore, the first contact surface 11 of the first plate 101 and the second contact surface 21 of the second plate 2 are melted by the heat which is stored up in the first plate 101.
  • However, the glass filler 102 of the first plate 101 cannot be melted by the heat of the laser beam, and the glass filler 102 therefore floats in the first kind of synthetic resin melted from the first plate 1 and the second kind of synthetic resin melted for the second plate 2 because the glass filler has a higher melting point than melting points of the first kind of synthetic resin and the second kind of synthetic. As a result, as shown in FIG. 6 and FIG. 7, a plurality of the fibers of the glass filler 102 will have ends in the first plate 101 and opposite ends in the second plate 2. Accordingly, some of the glass filler securely connects the first plate 101 to the second plate 2.
  • As shown in FIG. 10, the cohesiveness between the first plate 101 and the' second plate 2 increases as the wt% of the glass filler increases. The data in FIG. 10 was obtained by joining the preferred first and second kinds of synthetic resins by the heat of a Nd:YAG laser beam, whose generating power is 87W and whose wavelength is 1.06 pm.
  • Therefore, in the process of the second embodiment, the first kind of synthetic resin can be joined securely to the second kind of synthetic resin through the glass filler 102.
  • As has been described above, according to the process for joining different kinds of synthetic resins of the present invention, one kind of synthetic resin can be joined securely to a different kind of synthetic resin without any mechanical devices. Further techniques for joining different kinds of synthetic resins may be found in the applications owned by applicant's assignee, filed in the European Patent Office concurrently with the present application and all entitled "A Process for Joining Different Kinds of Synthetic Resins".
  • It should be apparent to one skilled in the art that the above-described embodiments are merely illustrations of a few of the many possible specific embodiments of the present invention. Numerous and varied other arrangements can readily be devised by those skilled in the art without departing from the spirit and scope of the invention, which is defined by the following claims.

Claims (9)

1. A process for joining an article (1) of a first kind of synthetic resin to an article (2) of a second kind of synthetic resin, by forming a bond between a first contact surface (11) of the first article (1) and a second contact surface (21) of the second article (2), characterized in that the second article (2) is adapted to transmit a laser beam (F1) to the first article (1), and the first article (1) is adapted to store up the heat of the laser beam, and an outer surface of the second article (2) is exposed to a laser beam, wherein the first contact surface (11) and the second contact surface (21) are melted, and joined together.
2. A process according to Claim 1, characterized in that the first kind of synthetic resin is styrene/ acrylonitrile copolymer or polypropylene resin, both having an absorptive additive.
3. A process according to Claim 2, characterized in that the additive of the styrene/acrylonitrile copolymer is carbon black.
4. A process according to any preceding Claim, characterized in that the second kind of synthetic resin is polypropylene resin, 6-nylon resin, 66-nylon resin or styrene/acrylonitrile copolymer, all being without any absorptive additives.
5. A process according to Claim 1 or -2, characterized in that the first article (101) has a plurality of fibrous fillers (102).
6. A process according to Claim 5, characterized in that, after the exposing step, at least some of the plurality qf fibrous fillers (102) have ends in the first article (101) and opposite ends in the second article (2), whereby at least some of the filler (102) connect the first article (101) to the second article (2).
7. A process according to Claim 5 or 6, characterized in that the fibrous fillers (102) comprise glass, metal or carbon fillers.
8. A process according to any preceding Claim, characterized in that the laser beam generated by a Nd:YAG laser, Nd:g1ass laser, ruby laser, helium: neon (He:Ne) gas laser, krypton (Kr) gas laser, argon (Ar) gas laser, hydrogen (H2) gas laser or nitrogen (N2) gas laser.
9. A process according to any preceding Claim, characterized in that the first and second contact surfaces (11,21) melt and form a plurality of projections and a plurality of recesses in each of the first and second contact surfaces (11,21) and engage to join together the first and second articles (1,2).
EP19850302432 1984-04-09 1985-04-04 A process for joining different kinds of synthetic resins Withdrawn EP0159169A3 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP59070606A JPS60214929A (en) 1984-04-09 1984-04-09 Bonding of different synthetic resin materials
JP70606/84 1984-04-09
JP72256/84 1984-04-10
JP59072256A JPS60214931A (en) 1984-04-10 1984-04-10 Bonding of different synthetic resin materials

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EP0159169A2 true EP0159169A2 (en) 1985-10-23
EP0159169A3 EP0159169A3 (en) 1987-07-01

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Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3621030A1 (en) * 1986-06-24 1988-01-07 Alkor Gmbh Process and device for welding and/or severing and welding by means of laser beams
GB2276584A (en) * 1993-04-01 1994-10-05 British Gas Plc Joining bodies of thermoplastic material
WO1997017189A1 (en) * 1995-11-08 1997-05-15 Alliedsignal Inc. Improved performance of vibration welded thermoplastic joints
US5874146A (en) * 1996-11-01 1999-02-23 Alliedsignal Inc. Performance of vibration welded thermoplastic joints
US5893959A (en) * 1994-03-31 1999-04-13 Marquardt Gmbh Workpiece of plastic and production process for such a workpiece
US6210507B1 (en) 1998-01-29 2001-04-03 Thermoform A/S Method for the manufacture of a plastic window
CN1076271C (en) * 1995-11-08 2001-12-19 联合讯号公司 Improved performance of vibration welded thermoplastic joints
WO2002010636A1 (en) 2000-08-01 2002-02-07 Ibs Filtran Kunststoff-/ Metallerzeugnisse Gmbh Oil reservoir and method for the production thereof
WO2002038677A2 (en) * 2000-11-10 2002-05-16 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
EP1334148A2 (en) * 2000-11-13 2003-08-13 E.I. Dupont De Nemours And Company Colored thermoplastic resin compositions for laser welding, colorants therefor of mixtures of amine salts of anthraquinone and monoazo complex dyes, and molded product therefrom
DE10207777A1 (en) * 2002-02-23 2003-09-11 A B Elektronik Gmbh Housing for angle sensor or rpm sensor, is made from laser opaque plastic and has cap made from laser-transparent plastic laser welded to it
EP1353991A1 (en) * 2000-11-13 2003-10-22 E.I. Dupont De Nemours And Company Colored thermoplastic resin compositions for laser welding, specific neutral anthraquinone dyes as colorants therefor, and molded product therefrom
DE10221303A1 (en) * 2002-05-14 2003-11-27 Valeo Schalter & Sensoren Gmbh Sensor, in particular ultrasound sensor, and method of manufacture
US6752893B2 (en) 2001-09-28 2004-06-22 Gentex Corporation Rimless spectacles and method for making the same
US6770158B2 (en) 2002-01-15 2004-08-03 Gentex Corporation Quality management system for pre-processed workpiece
US6960027B1 (en) 1999-04-28 2005-11-01 Tyco Electronics Logistics Ag Method of fixing a ferrule to an optical waveguide
US6974207B2 (en) * 2002-11-19 2005-12-13 Lexmark International, Inc. Laser welding methods and structures and control therefor including welded inkjet printheads
US6980296B2 (en) 2003-01-30 2005-12-27 Lexmark International, Inc. Measuring laser light transmissivity in a to-be-welded region of a work piece
WO2006089534A1 (en) 2005-02-21 2006-08-31 Airbus Deutschland Gmbh Fiber composite component and method for the production of a fiber composite component
US7244330B2 (en) 2004-09-02 2007-07-17 Hellermann Tyton Gmbh Method for bonding a layer of thermoplastic polymer to the surface of an elastomer
DE102008020943A1 (en) 2008-04-25 2009-10-29 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Method for joining at least two transparent joining partners by means of laser transmission welding
CN101128307B (en) * 2005-02-21 2010-10-13 空中客车德国有限公司 Fiber composite structure component and method for producing the fiber composite structure component
DE10059160B4 (en) * 2000-01-25 2010-12-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Flat vehicle component, namely bumper, door or fender trim or boot lid
US7875147B2 (en) 2004-04-14 2011-01-25 Basf Akiengesellschaft Method for welding together plastic parts with the aid of laser radiation
DE102011107537A1 (en) 2010-07-27 2012-02-02 Marquardt Gmbh Method for welding two parts of housing element with joint surface using laser radiation in region of motor car, involves pressing parts at joint surface opposite to each other until joint surface is cooled
FR3044369A1 (en) * 2015-12-01 2017-06-02 Valeo Embrayages SENSOR ASSEMBLY FOR HYDRAULIC CONTROL DEVICE
WO2017153493A1 (en) 2016-03-11 2017-09-14 Aft Automotive Gmbh Method for producing a moulded part assembly and corresponding production device
US9945389B2 (en) 2014-05-05 2018-04-17 Horton, Inc. Composite fan
EP2923821B1 (en) 2014-03-28 2019-08-07 Sogefi Engine Systems USA, Inc. Method for direct infrared laser welding
CN111448076A (en) * 2017-12-08 2020-07-24 株式会社普利司通 Tyre for vehicle wheels

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GB1051397A (en) * 1964-11-19 1966-12-14
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DE1958430A1 (en) * 1969-11-21 1971-05-27 Dozler Geb Bauscher Elisabeth Welding device

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Cited By (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3621030A1 (en) * 1986-06-24 1988-01-07 Alkor Gmbh Process and device for welding and/or severing and welding by means of laser beams
GB2276584A (en) * 1993-04-01 1994-10-05 British Gas Plc Joining bodies of thermoplastic material
GB2276584B (en) * 1993-04-01 1997-09-17 British Gas Plc Joining bodies of thermoplastic material
US5888331A (en) * 1993-04-01 1999-03-30 Bg Plc Joining bodies of thermoplastic material
US5893959A (en) * 1994-03-31 1999-04-13 Marquardt Gmbh Workpiece of plastic and production process for such a workpiece
EP0751865B2 (en) 1994-03-31 2004-07-14 Marquardt GmbH Plastic workpiece and process for producing it
CN1076271C (en) * 1995-11-08 2001-12-19 联合讯号公司 Improved performance of vibration welded thermoplastic joints
WO1997017189A1 (en) * 1995-11-08 1997-05-15 Alliedsignal Inc. Improved performance of vibration welded thermoplastic joints
US5874146A (en) * 1996-11-01 1999-02-23 Alliedsignal Inc. Performance of vibration welded thermoplastic joints
US6210507B1 (en) 1998-01-29 2001-04-03 Thermoform A/S Method for the manufacture of a plastic window
US6960027B1 (en) 1999-04-28 2005-11-01 Tyco Electronics Logistics Ag Method of fixing a ferrule to an optical waveguide
DE10059160B4 (en) * 2000-01-25 2010-12-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Flat vehicle component, namely bumper, door or fender trim or boot lid
WO2002010636A1 (en) 2000-08-01 2002-02-07 Ibs Filtran Kunststoff-/ Metallerzeugnisse Gmbh Oil reservoir and method for the production thereof
WO2002038677A2 (en) * 2000-11-10 2002-05-16 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
WO2002038677A3 (en) * 2000-11-10 2002-07-11 Gentex Corp Visibly transparent dyes for through-transmission laser welding
US7276136B2 (en) 2000-11-10 2007-10-02 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
US6911262B2 (en) 2000-11-10 2005-06-28 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
US6656315B2 (en) 2000-11-10 2003-12-02 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
EP1334148A2 (en) * 2000-11-13 2003-08-13 E.I. Dupont De Nemours And Company Colored thermoplastic resin compositions for laser welding, colorants therefor of mixtures of amine salts of anthraquinone and monoazo complex dyes, and molded product therefrom
EP1353991A1 (en) * 2000-11-13 2003-10-22 E.I. Dupont De Nemours And Company Colored thermoplastic resin compositions for laser welding, specific neutral anthraquinone dyes as colorants therefor, and molded product therefrom
EP1353990A4 (en) * 2000-11-13 2004-12-15 Du Pont Colored thermoplastic resin compositions for laser welding, specific neutral anthraquinone dyes as colorants therefor, and molded product therefrom
EP1334148A4 (en) * 2000-11-13 2004-12-15 Du Pont Colored thermoplastic resin compositions for laser welding, colorants therefor of mixtures of amine salts of anthraquinone and monoazo complex dyes, and molded product therefrom
EP1353991A4 (en) * 2000-11-13 2005-01-19 Du Pont Colored thermoplastic resin compositions for laser welding, specific neutral anthraquinone dyes as colorants therefor, and molded product therefrom
EP1353990A2 (en) * 2000-11-13 2003-10-22 E.I. Du Pont De Nemours And Company Colored thermoplastic resin compositions for laser welding, specific neutral anthraquinone dyes as colorants therefor, and molded product therefrom
US6752893B2 (en) 2001-09-28 2004-06-22 Gentex Corporation Rimless spectacles and method for making the same
US6770158B2 (en) 2002-01-15 2004-08-03 Gentex Corporation Quality management system for pre-processed workpiece
US7344774B2 (en) 2002-01-15 2008-03-18 Gentex Corporation Pre-processed workpiece having a surface deposition of absorber dye rendering the workpiece weld-enabled
US7201963B2 (en) 2002-01-15 2007-04-10 Gentex Corporation Pre-processed workpiece having a surface deposition of absorber dye rendering the workpiece weld-enabled
DE10207777A1 (en) * 2002-02-23 2003-09-11 A B Elektronik Gmbh Housing for angle sensor or rpm sensor, is made from laser opaque plastic and has cap made from laser-transparent plastic laser welded to it
DE10221303A1 (en) * 2002-05-14 2003-11-27 Valeo Schalter & Sensoren Gmbh Sensor, in particular ultrasound sensor, and method of manufacture
US6974207B2 (en) * 2002-11-19 2005-12-13 Lexmark International, Inc. Laser welding methods and structures and control therefor including welded inkjet printheads
US7354137B2 (en) * 2002-11-19 2008-04-08 Lexmark International, Inc. Laser welding methods and structures and control therefor including welded inkjet printheads
US6980296B2 (en) 2003-01-30 2005-12-27 Lexmark International, Inc. Measuring laser light transmissivity in a to-be-welded region of a work piece
US7245378B2 (en) 2003-01-30 2007-07-17 Lexmark International, Inc. Measuring laser light transmissivity in a to-be-welded region of a work piece
US7875147B2 (en) 2004-04-14 2011-01-25 Basf Akiengesellschaft Method for welding together plastic parts with the aid of laser radiation
US7244330B2 (en) 2004-09-02 2007-07-17 Hellermann Tyton Gmbh Method for bonding a layer of thermoplastic polymer to the surface of an elastomer
US8551381B2 (en) 2005-02-21 2013-10-08 Airbus Deutschland Gmbh Fiber composite component and method for the production of a fiber composite component
WO2006089534A1 (en) 2005-02-21 2006-08-31 Airbus Deutschland Gmbh Fiber composite component and method for the production of a fiber composite component
CN101128307B (en) * 2005-02-21 2010-10-13 空中客车德国有限公司 Fiber composite structure component and method for producing the fiber composite structure component
DE102008020943A1 (en) 2008-04-25 2009-10-29 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Method for joining at least two transparent joining partners by means of laser transmission welding
DE102011107537A1 (en) 2010-07-27 2012-02-02 Marquardt Gmbh Method for welding two parts of housing element with joint surface using laser radiation in region of motor car, involves pressing parts at joint surface opposite to each other until joint surface is cooled
EP2923821B1 (en) 2014-03-28 2019-08-07 Sogefi Engine Systems USA, Inc. Method for direct infrared laser welding
US9945389B2 (en) 2014-05-05 2018-04-17 Horton, Inc. Composite fan
US10415587B2 (en) 2014-05-05 2019-09-17 Horton, Inc. Composite fan and method of manufacture
US10914314B2 (en) 2014-05-05 2021-02-09 Horton, Inc. Modular fan assembly
FR3044369A1 (en) * 2015-12-01 2017-06-02 Valeo Embrayages SENSOR ASSEMBLY FOR HYDRAULIC CONTROL DEVICE
WO2017153493A1 (en) 2016-03-11 2017-09-14 Aft Automotive Gmbh Method for producing a moulded part assembly and corresponding production device
CN111448076A (en) * 2017-12-08 2020-07-24 株式会社普利司通 Tyre for vehicle wheels
US11679628B2 (en) 2017-12-08 2023-06-20 Bridgestone Corporation Tire

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